RU2016102180A3 - - Google Patents
Download PDFInfo
- Publication number
- RU2016102180A3 RU2016102180A3 RU2016102180A RU2016102180A RU2016102180A3 RU 2016102180 A3 RU2016102180 A3 RU 2016102180A3 RU 2016102180 A RU2016102180 A RU 2016102180A RU 2016102180 A RU2016102180 A RU 2016102180A RU 2016102180 A3 RU2016102180 A3 RU 2016102180A3
- Authority
- RU
- Russia
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
- F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
- F01D5/189—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/14—Casings modified therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/002—Wall structures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/10—Two-dimensional
- F05D2250/18—Two-dimensional patterned
- F05D2250/185—Two-dimensional patterned serpentine-like
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/204—Heat transfer, e.g. cooling by the use of microcircuits
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/03043—Convection cooled combustion chamber walls with means for guiding the cooling air flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/03045—Convection cooled combustion chamber walls provided with turbolators or means for creating turbulences to increase cooling
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2016102180A RU2706211C2 (ru) | 2016-01-25 | 2016-01-25 | Охлаждаемая стенка компонента турбины и способ охлаждения этой стенки |
KR1020170011039A KR20170088770A (ko) | 2016-01-25 | 2017-01-24 | 터빈 구성 요소의 냉각 벽 및 상기 벽을 냉각시키는 방법 |
JP2017011096A JP2017172578A (ja) | 2016-01-25 | 2017-01-25 | タービン構成要素の冷却壁及びこの壁を冷却する方法 |
EP17153155.1A EP3199761B1 (en) | 2016-01-25 | 2017-01-25 | A cooled wall of a turbine component and a method for cooling this wall |
CN201710275549.5A CN107091123B (zh) | 2016-01-25 | 2017-01-25 | 涡轮机部件的冷却壁及冷却该壁的方法 |
US15/415,413 US10851668B2 (en) | 2016-01-25 | 2017-01-25 | Cooled wall of a turbine component and a method for cooling this wall |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2016102180A RU2706211C2 (ru) | 2016-01-25 | 2016-01-25 | Охлаждаемая стенка компонента турбины и способ охлаждения этой стенки |
Publications (3)
Publication Number | Publication Date |
---|---|
RU2016102180A RU2016102180A (ru) | 2017-07-28 |
RU2016102180A3 true RU2016102180A3 (es) | 2019-06-13 |
RU2706211C2 RU2706211C2 (ru) | 2019-11-14 |
Family
ID=57906511
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2016102180A RU2706211C2 (ru) | 2016-01-25 | 2016-01-25 | Охлаждаемая стенка компонента турбины и способ охлаждения этой стенки |
Country Status (6)
Country | Link |
---|---|
US (1) | US10851668B2 (es) |
EP (1) | EP3199761B1 (es) |
JP (1) | JP2017172578A (es) |
KR (1) | KR20170088770A (es) |
CN (1) | CN107091123B (es) |
RU (1) | RU2706211C2 (es) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20180223673A1 (en) * | 2017-02-07 | 2018-08-09 | General Electric Company | Hot gas path component with metering structure including converging-diverging passage portions |
US20190003320A1 (en) * | 2017-06-30 | 2019-01-03 | General Electric Company | Turbomachine rotor blade |
CN108644018B (zh) * | 2018-04-24 | 2021-03-12 | 西安交通大学 | 一种具有提高端壁冷却效率的异型槽缝冷却结构 |
DE102018210598A1 (de) * | 2018-06-28 | 2020-01-02 | MTU Aero Engines AG | Gehäusestruktur für eine Strömungsmaschine, Strömungsmaschine und Verfahren zum Kühlen eines Gehäuseabschnitts einer Gehäusestruktur einer Strömungsmaschine |
EP3674519A1 (en) * | 2018-12-27 | 2020-07-01 | Siemens Aktiengesellschaft | Coolable component for a streaming engine and corresponding manufacturing method |
CN112177682B (zh) * | 2020-09-29 | 2021-08-10 | 大连理工大学 | 一种采用波浪式隔肋的涡轮叶片尾缘劈缝冷却结构 |
CN113074387B (zh) * | 2021-04-29 | 2022-02-25 | 北京航空航天大学 | 一种带有桁架结构的再生冷却通道 |
CN113669759A (zh) * | 2021-09-13 | 2021-11-19 | 中国联合重型燃气轮机技术有限公司 | 用于燃气轮机的罩帽 |
KR102636366B1 (ko) * | 2021-09-15 | 2024-02-13 | 두산에너빌리티 주식회사 | 링 세그먼트, 이를 포함하는 회전 기계 |
CN115045721B (zh) * | 2022-08-17 | 2022-12-06 | 中国航发四川燃气涡轮研究院 | 一种串联式旋流冲击涡轮叶片冷却单元及涡轮叶片 |
GB2621852A (en) * | 2022-08-24 | 2024-02-28 | Siemens Energy Global Gmbh & Co Kg | Turbine vane for a gas turbine |
US20240125243A1 (en) * | 2022-10-13 | 2024-04-18 | Raytheon Technologies Corporation | Cooling features for a component of a gas turbine engine |
EP4372281A1 (en) * | 2022-11-18 | 2024-05-22 | ANSALDO ENERGIA S.p.A. | Combustion chamber for a power plant gas turbine assembly comprising a plurality of metallic heat shielding tiles with improved air cooling feature |
Family Cites Families (52)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3767322A (en) | 1971-07-30 | 1973-10-23 | Westinghouse Electric Corp | Internal cooling for turbine vanes |
SU444888A1 (ru) * | 1973-01-03 | 1974-09-30 | Предприятие П/Я В-2504 | Охлаждаема лопатка турбины |
SU779590A1 (ru) * | 1977-07-21 | 1980-11-15 | Предприятие П/Я А-1469 | Охлаждаема лопатка турбины |
US4835958A (en) * | 1978-10-26 | 1989-06-06 | Rice Ivan G | Process for directing a combustion gas stream onto rotatable blades of a gas turbine |
US4302940A (en) * | 1979-06-13 | 1981-12-01 | General Motors Corporation | Patterned porous laminated material |
US4297077A (en) | 1979-07-09 | 1981-10-27 | Westinghouse Electric Corp. | Cooled turbine vane |
US4312186A (en) * | 1979-10-17 | 1982-01-26 | General Motors Corporation | Shingled laminated porous material |
FR2678318B1 (fr) | 1991-06-25 | 1993-09-10 | Snecma | Aube refroidie de distributeur de turbine. |
US5375973A (en) * | 1992-12-23 | 1994-12-27 | United Technologies Corporation | Turbine blade outer air seal with optimized cooling |
US5363654A (en) * | 1993-05-10 | 1994-11-15 | General Electric Company | Recuperative impingement cooling of jet engine components |
US5328331A (en) * | 1993-06-28 | 1994-07-12 | General Electric Company | Turbine airfoil with double shell outer wall |
US5374161A (en) * | 1993-12-13 | 1994-12-20 | United Technologies Corporation | Blade outer air seal cooling enhanced with inter-segment film slot |
RU2062954C1 (ru) * | 1994-06-16 | 1996-06-27 | Акционерное общество "Авиадвигатель" | Жаровая труба камеры сгорания газотурбинного двигателя |
US5737922A (en) * | 1995-01-30 | 1998-04-14 | Aerojet General Corporation | Convectively cooled liner for a combustor |
US5538393A (en) * | 1995-01-31 | 1996-07-23 | United Technologies Corporation | Turbine shroud segment with serpentine cooling channels having a bend passage |
US5933699A (en) * | 1996-06-24 | 1999-08-03 | General Electric Company | Method of making double-walled turbine components from pre-consolidated assemblies |
US5975850A (en) * | 1996-12-23 | 1999-11-02 | General Electric Company | Turbulated cooling passages for turbine blades |
FR2765265B1 (fr) | 1997-06-26 | 1999-08-20 | Snecma | Aubage refroidi par rampe helicoidale, par impact en cascade et par systeme a pontets dans une double peau |
JP3368417B2 (ja) * | 1997-12-25 | 2003-01-20 | 株式会社日立製作所 | タービン静翼 |
CA2288557C (en) * | 1998-11-12 | 2007-02-06 | Mitsubishi Heavy Industries, Ltd. | Gas turbine combustor cooling structure |
GB2365930B (en) * | 2000-08-12 | 2004-12-08 | Rolls Royce Plc | A turbine blade support assembly and a turbine assembly |
GB0117110D0 (en) * | 2001-07-13 | 2001-09-05 | Siemens Ag | Coolable segment for a turbomachinery and combustion turbine |
US6761031B2 (en) | 2002-09-18 | 2004-07-13 | General Electric Company | Double wall combustor liner segment with enhanced cooling |
DE10253852A1 (de) * | 2002-11-19 | 2004-06-09 | Bayer Ag | Thermoplastischer Wärmetauscher |
DE10318061A1 (de) * | 2003-04-17 | 2004-10-28 | Behr Gmbh & Co. Kg | Mischvorrichtung |
US6905302B2 (en) * | 2003-09-17 | 2005-06-14 | General Electric Company | Network cooled coated wall |
US7118326B2 (en) | 2004-06-17 | 2006-10-10 | Siemens Power Generation, Inc. | Cooled gas turbine vane |
US20070029369A1 (en) * | 2005-08-02 | 2007-02-08 | United Technologies Corporation | Transient liquid phase bonding of dissimilar metals |
US7740161B2 (en) * | 2005-09-06 | 2010-06-22 | Volvo Aero Corporation | Engine wall structure and a method of producing an engine wall structure |
SE529516C2 (sv) * | 2005-10-24 | 2007-09-04 | Alfa Laval Corp Ab | Universell flödesmodul |
US7535072B2 (en) * | 2006-01-18 | 2009-05-19 | Hannstar Display Corporation | Input display |
US7497655B1 (en) | 2006-08-21 | 2009-03-03 | Florida Turbine Technologies, Inc. | Turbine airfoil with near-wall impingement and vortex cooling |
US7563072B1 (en) | 2006-09-25 | 2009-07-21 | Florida Turbine Technologies, Inc. | Turbine airfoil with near-wall spiral flow cooling circuit |
US20100037620A1 (en) | 2008-08-15 | 2010-02-18 | General Electric Company, Schenectady | Impingement and effusion cooled combustor component |
US20100236245A1 (en) * | 2009-03-19 | 2010-09-23 | Johnson Clifford E | Gas Turbine Combustion System |
EP2256297B8 (en) | 2009-05-19 | 2012-10-03 | Alstom Technology Ltd | Gas turbine vane with improved cooling |
KR100938802B1 (ko) * | 2009-06-11 | 2010-01-27 | 국방과학연구소 | 마이크로채널 열교환기 |
US8268233B2 (en) * | 2009-10-16 | 2012-09-18 | Macrae Allan J | Eddy-free high velocity cooler |
US8444386B1 (en) * | 2010-01-19 | 2013-05-21 | Florida Turbine Technologies, Inc. | Turbine blade with multiple near wall serpentine flow cooling |
US8550778B2 (en) * | 2010-04-20 | 2013-10-08 | Mitsubishi Heavy Industries, Ltd. | Cooling system of ring segment and gas turbine |
US8727704B2 (en) * | 2010-09-07 | 2014-05-20 | Siemens Energy, Inc. | Ring segment with serpentine cooling passages |
EP2444769A1 (en) * | 2010-10-18 | 2012-04-25 | Kryoz Technologies B.V. | Micro-cooling device |
US8608430B1 (en) | 2011-06-27 | 2013-12-17 | Florida Turbine Technologies, Inc. | Turbine vane with near wall multiple impingement cooling |
CN102393144B (zh) * | 2011-10-18 | 2013-09-25 | 绍兴曙光机械有限公司 | 一种埋双层纯铜管铸铜水套制造方法 |
US20130243575A1 (en) * | 2012-03-13 | 2013-09-19 | United Technologies Corporation | Cooling pedestal array |
US8414263B1 (en) | 2012-03-22 | 2013-04-09 | Florida Turbine Technologies, Inc. | Turbine stator vane with near wall integrated micro cooling channels |
EP2685171B1 (en) * | 2012-07-09 | 2018-03-21 | Ansaldo Energia Switzerland AG | Burner arrangement |
EP2738469B1 (en) * | 2012-11-30 | 2019-04-17 | Ansaldo Energia IP UK Limited | Combustor part of a gas turbine comprising a near wall cooling arrangement |
US20140238642A1 (en) * | 2013-02-26 | 2014-08-28 | Pratt & Whitney Canada Corp. | Heat exchange device and method |
EP2860358A1 (en) * | 2013-10-10 | 2015-04-15 | Alstom Technology Ltd | Arrangement for cooling a component in the hot gas path of a gas turbine |
US9777963B2 (en) * | 2014-06-30 | 2017-10-03 | General Electric Company | Method and system for radial tubular heat exchangers |
US10480787B2 (en) * | 2015-03-26 | 2019-11-19 | United Technologies Corporation | Combustor wall cooling channel formed by additive manufacturing |
-
2016
- 2016-01-25 RU RU2016102180A patent/RU2706211C2/ru active
-
2017
- 2017-01-24 KR KR1020170011039A patent/KR20170088770A/ko unknown
- 2017-01-25 CN CN201710275549.5A patent/CN107091123B/zh active Active
- 2017-01-25 EP EP17153155.1A patent/EP3199761B1/en active Active
- 2017-01-25 US US15/415,413 patent/US10851668B2/en active Active
- 2017-01-25 JP JP2017011096A patent/JP2017172578A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
CN107091123B (zh) | 2021-10-22 |
RU2706211C2 (ru) | 2019-11-14 |
US20170211418A1 (en) | 2017-07-27 |
JP2017172578A (ja) | 2017-09-28 |
EP3199761B1 (en) | 2019-07-24 |
EP3199761A1 (en) | 2017-08-02 |
KR20170088770A (ko) | 2017-08-02 |
RU2016102180A (ru) | 2017-07-28 |
CN107091123A (zh) | 2017-08-25 |
US10851668B2 (en) | 2020-12-01 |